removing the tabs in folders.

Author: WallyMaier

Common/include/geometry/CGeometry.hpp

@@ -84,7 +84,7 @@ class CGeometry {
   nPointGhost{0},                 /*!< \brief Number of ghost points of the mesh. */
   nPointNode{0},                  /*!< \brief Size of the node array allocated to hold CPoint objects. */
   Global_nPoint{0},               /*!< \brief Total number of nodes in a simulation across all processors (including halos). */
-  Global_nPointDomain{0},	        /*!< \brief Total number of nodes in a simulation across all processors (excluding halos). */
+  Global_nPointDomain{0},         /*!< \brief Total number of nodes in a simulation across all processors (excluding halos). */
   nElem{0},                       /*!< \brief Number of elements of the mesh. */
   Global_nElem{0},                /*!< \brief Total number of elements in a simulation across all processors (all types). */
   Global_nElemDomain{0},          /*!< \brief Total number of elements in a simulation across all processors (excluding halos). */
@@ -189,7 +189,7 @@ class CGeometry {
 
   CPrimalGrid** elem{nullptr};           /*!< \brief Element vector (primal grid information). */
   CPrimalGrid** face{nullptr};           /*!< \brief Face vector (primal grid information). */
-  CPrimalGrid*** bound{nullptr};	       /*!< \brief Boundary vector (primal grid information). */
+  CPrimalGrid*** bound{nullptr};         /*!< \brief Boundary vector (primal grid information). */
   CPoint* nodes{nullptr};                /*!< \brief Node vector (dual grid information). */
   CEdge* edges{nullptr};                 /*!< \brief Edge vector (dual grid information). */
   CVertex*** vertex{nullptr};            /*!< \brief Boundary Vertex vector (dual grid information). */

Common/include/option_structure.hpp

@@ -64,12 +64,12 @@ using MapType = CEmptyMap<T,U>;
  * \brief Different software components of SU2
  */
 enum SU2_COMPONENT {
-  SU2_CFD = 1,	/*!< \brief Running the SU2_CFD software. */
-  SU2_DEF = 2,	/*!< \brief Running the SU2_DEF software. */
-  SU2_DOT = 3,	/*!< \brief Running the SU2_DOT software. */
-  SU2_MSH = 4,	/*!< \brief Running the SU2_MSH software. */
-  SU2_GEO = 5,	/*!< \brief Running the SU2_GEO software. */
-  SU2_SOL = 6 	/*!< \brief Running the SU2_SOL software. */
+  SU2_CFD = 1,  /*!< \brief Running the SU2_CFD software. */
+  SU2_DEF = 2,  /*!< \brief Running the SU2_DEF software. */
+  SU2_DOT = 3,  /*!< \brief Running the SU2_DOT software. */
+  SU2_MSH = 4,  /*!< \brief Running the SU2_MSH software. */
+  SU2_GEO = 5,  /*!< \brief Running the SU2_GEO software. */
+  SU2_SOL = 6   /*!< \brief Running the SU2_SOL software. */
 };
 
 const unsigned int EXIT_DIVERGENCE = 2;   /*!< \brief Exit code (divergence). */
@@ -110,9 +110,9 @@ const su2double PI_NUMBER = 4.0 * atan(1.0);  /*!< \brief Pi number. */
 
 const su2double STEFAN_BOLTZMANN = 5.670367E-08;  /*!< \brief Stefan-Boltzmann constant in W/(m^2*K^4). */
 
-const int MASTER_NODE = 0;			/*!< \brief Master node for MPI parallelization. */
-const int SINGLE_NODE = 1;			/*!< \brief There is only a node in the MPI parallelization. */
-const int SINGLE_ZONE = 1;			/*!< \brief There is only a zone. */
+const int MASTER_NODE = 0;      /*!< \brief Master node for MPI parallelization. */
+const int SINGLE_NODE = 1;      /*!< \brief There is only a node in the MPI parallelization. */
+const int SINGLE_ZONE = 1;      /*!< \brief There is only a zone. */
 
 const unsigned short COMM_TYPE_UNSIGNED_LONG  = 1;  /*!< \brief Communication type for unsigned long. */
 const unsigned short COMM_TYPE_LONG           = 2;  /*!< \brief Communication type for long. */
@@ -400,8 +400,8 @@ enum ENUM_TRANSFER {
  * \brief different regime modes
  */
 enum ENUM_REGIME {
-  COMPRESSIBLE = 0,		/*!< \brief Definition of compressible solver. */
-  INCOMPRESSIBLE = 1,	/*!< \brief Definition of incompressible solver. */
+  COMPRESSIBLE = 0,   /*!< \brief Definition of compressible solver. */
+  INCOMPRESSIBLE = 1, /*!< \brief Definition of incompressible solver. */
   NO_FLOW = 2
 };
 
@@ -429,8 +429,8 @@ static const MapType<string, ENUM_KIND_NONDIM> NonDim_Map = {
  * \brief different system of measurements
  */
 enum ENUM_MEASUREMENTS {
-  SI = 0,			/*!< \brief Definition of compressible solver. */
-  US = 1			/*!< \brief Definition of incompressible solver. */
+  SI = 0,     /*!< \brief Definition of compressible solver. */
+  US = 1      /*!< \brief Definition of incompressible solver. */
 };
 static const MapType<string, ENUM_MEASUREMENTS> Measurements_Map = {
   MakePair("SI", SI)
@@ -1268,7 +1268,7 @@ enum RIEMANN_TYPE {
   TOTAL_CONDITIONS_PT = 1,          /*!< \brief User specifies total pressure, total temperature, and flow direction. */
   DENSITY_VELOCITY = 2,             /*!< \brief User specifies density and velocity, and flow direction. */
   STATIC_PRESSURE = 3,              /*!< \brief User specifies static pressure. */
-  TOTAL_SUPERSONIC_INFLOW = 4,	    /*!< \brief User specifies total pressure, total temperature and Velocity components. */
+  TOTAL_SUPERSONIC_INFLOW = 4,      /*!< \brief User specifies total pressure, total temperature and Velocity components. */
   STATIC_SUPERSONIC_INFLOW_PT = 5,  /*!< \brief User specifies static pressure, static temperature, and Mach components. */
   STATIC_SUPERSONIC_INFLOW_PD = 6,  /*!< \brief User specifies static pressure, static temperature, and Mach components. */
   MIXING_IN = 7,                    /*!< \brief User does not specify anything; information is retrieved from the other domain */
@@ -1320,7 +1320,7 @@ static const MapType<string, RIEMANN_TYPE> Giles_Map = {
 enum AVERAGEPROCESS_TYPE {
   ALGEBRAIC = 1,  /*!< \brief an algebraic average is computed at the boundary of interest. */
   AREA = 2,       /*!< \brief an area average is computed at the boundary of interest. */
-  MIXEDOUT = 3,	  /*!< \brief an mixed-out average is computed at the boundary of interest. */
+  MIXEDOUT = 3,   /*!< \brief an mixed-out average is computed at the boundary of interest. */
   MASSFLUX = 4    /*!< \brief a mass flow average is computed at the boundary of interest. */
 };
 static const MapType<string, AVERAGEPROCESS_TYPE> AverageProcess_Map = {
@@ -1378,15 +1378,15 @@ static const MapType<string, TURBOMACHINERY_TYPE> TurboMachinery_Map = {
  * \brief Types of Turbomachinery performance flag.
  */
 enum TURBO_MARKER_TYPE{
-  INFLOW   = 1,	  /*!< \brief flag for inflow marker for compute turboperformance. */
+  INFLOW  = 1,    /*!< \brief flag for inflow marker for compute turboperformance. */
   OUTFLOW = 2     /*!< \brief flag for outflow marker for compute turboperformance. */
 };
 
 /*!
  * \brief Types inlet boundary treatments
  */
 enum INLET_TYPE {
-  TOTAL_CONDITIONS = 1,	  /*!< \brief User specifies total pressure, total temperature, and flow direction. */
+  TOTAL_CONDITIONS = 1,   /*!< \brief User specifies total pressure, total temperature, and flow direction. */
   MASS_FLOW = 2,          /*!< \brief User specifies density and velocity (mass flow). */
   INPUT_FILE = 3,         /*!< \brief User specifies an input file. */
   VELOCITY_INLET = 4,     /*!< \brief Velocity inlet for an incompressible flow. */
@@ -1482,7 +1482,7 @@ enum ENUM_OBJECTIVE {
   LIFT_COEFFICIENT = 2,         /*!< \brief Lift objective function definition. */
   SIDEFORCE_COEFFICIENT = 3,    /*!< \brief Side force objective function definition. */
   EFFICIENCY = 4,               /*!< \brief Efficiency objective function definition. */
-  INVERSE_DESIGN_PRESSURE = 5,	/*!< \brief Pressure objective function definition (inverse design). */
+  INVERSE_DESIGN_PRESSURE = 5,  /*!< \brief Pressure objective function definition (inverse design). */
   INVERSE_DESIGN_HEATFLUX = 6,  /*!< \brief Heat flux objective function definition (inverse design). */
   TOTAL_HEATFLUX = 7,           /*!< \brief Total heat flux. */
   MAXIMUM_HEATFLUX = 8,         /*!< \brief Maximum heat flux. */
@@ -1507,8 +1507,8 @@ enum ENUM_OBJECTIVE {
   SURFACE_SECONDARY = 53,       /*!< \brief Secondary flow strength objective function definition. */
   SURFACE_MOM_DISTORTION = 54,  /*!< \brief Momentum distortion objective function definition. */
   SURFACE_SECOND_OVER_UNIFORM = 55, /*!< \brief Secondary over uniformity (relative secondary strength) objective function definition. */
-  SURFACE_PRESSURE_DROP = 56, 	/*!< \brief Pressure drop objective function definition. */
-  CUSTOM_OBJFUNC = 31, 	        /*!< \brief Custom objective function definition. */
+  SURFACE_PRESSURE_DROP = 56,   /*!< \brief Pressure drop objective function definition. */
+  CUSTOM_OBJFUNC = 31,          /*!< \brief Custom objective function definition. */
   TOTAL_PRESSURE_LOSS = 39,
   KINETIC_ENERGY_LOSS = 40,
   TOTAL_EFFICIENCY = 41,
@@ -1582,8 +1582,8 @@ static const MapType<string, ENUM_OBJECTIVE> Objective_Map = {
  * \brief Types of residual criteria equations
  */
 enum ENUM_RESIDUAL {
-    RHO_RESIDUAL = 1, 	     /*!< \brief Rho equation residual criteria equation. */
-    RHO_ENERGY_RESIDUAL = 2  /*!< \brief RhoE equation residual criteria equation. */
+  RHO_RESIDUAL = 1,        /*!< \brief Rho equation residual criteria equation. */
+  RHO_ENERGY_RESIDUAL = 2  /*!< \brief RhoE equation residual criteria equation. */
 };
 static const MapType<string, ENUM_RESIDUAL> Residual_Map = {
   MakePair("RHO", RHO_RESIDUAL)
@@ -2029,7 +2029,7 @@ static const MapType<string, ENUM_GEO_ANALYTIC> Geo_Analytic_Map = {
  */
 enum ENUM_GEO_DESCRIPTION {
   TWOD_AIRFOIL = 0, /*!< \brief Airfoil analysis. */
-  WING = 1, 	    /*!< \brief Wing analysis. */
+  WING = 1,         /*!< \brief Wing analysis. */
   FUSELAGE = 2,     /*!< \brief Fuselage analysis. */
   NACELLE = 3       /*!< \brief Nacelle analysis. */
 };
@@ -2046,8 +2046,8 @@ static const MapType<string, ENUM_GEO_DESCRIPTION> Geo_Description_Map = {
 enum ENUM_UNSTEADY {
   STEADY = 0,            /*!< \brief A steady computation. */
   TIME_STEPPING = 1,     /*!< \brief Use a time stepping strategy for unsteady computations. */
-  DT_STEPPING_1ST = 2,	 /*!< \brief Use a dual time stepping strategy for unsteady computations (1st order). */
-  DT_STEPPING_2ND = 3,	 /*!< \brief Use a dual time stepping strategy for unsteady computations (2nd order). */
+  DT_STEPPING_1ST = 2,   /*!< \brief Use a dual time stepping strategy for unsteady computations (1st order). */
+  DT_STEPPING_2ND = 3,   /*!< \brief Use a dual time stepping strategy for unsteady computations (2nd order). */
   ROTATIONAL_FRAME = 4,  /*!< \brief Use a rotational source term. */
   HARMONIC_BALANCE = 5   /*!< \brief Use a harmonic balance source term. */
 };

Common/src/geometry/CPhysicalGeometry.cpp

@@ -5088,7 +5088,7 @@ unsigned short iMarker, jMarker, iMarkerTP, iSpan, jSpan, kSpan = 0;
   if (nDim == 2){
     nSpanWiseSections[marker_flag-1] = 1;
     //TODO (turbo) make it more genral
-    if(marker_flag == OUTFLOW)	config->SetnSpanWiseSections(1);
+    if(marker_flag == OUTFLOW) config->SetnSpanWiseSections(1);
 
     /*---Initilize the vector of span-wise values that will be ordered ---*/
     SpanWiseValue[marker_flag -1] = new su2double[1];
@@ -5154,7 +5154,7 @@ unsigned short iMarker, jMarker, iMarkerTP, iSpan, jSpan, kSpan = 0;
                 for (jMarker = 0; jMarker < nMarker; jMarker++){
                   if (config->GetMarker_All_KindBC(jMarker) == PERIODIC_BOUNDARY) {
                     PeriodicBoundary = config->GetMarker_All_PerBound(jMarker);
-                  	jVertex = nodes->GetVertex(iPoint, jMarker);
+                    jVertex = nodes->GetVertex(iPoint, jMarker);
                     if ((jVertex != -1) && (PeriodicBoundary == (val_iZone + 1))){
                       coord = nodes->GetCoord(iPoint);
                       switch (config->GetKind_TurboMachinery(val_iZone)){
@@ -5234,9 +5234,9 @@ unsigned short iMarker, jMarker, iMarkerTP, iSpan, jSpan, kSpan = 0;
       // check if the value are gathered correctly
       //
       //  for (iSpan = 0; iSpan < nSpan; iSpan++){
-      //  	if(rank == MASTER_NODE){
-      //  		cout << setprecision(16)<<  iSpan +1 << " with a value of " <<valueSpan[iSpan]<< " at flag " << marker_flag <<endl;
-      //  	}
+      //    if(rank == MASTER_NODE){
+      //      cout << setprecision(16)<<  iSpan +1 << " with a value of " <<valueSpan[iSpan]<< " at flag " << marker_flag <<endl;
+      //    }
       //  }
 
 

Common/src/geometry/elements/CHEXA8.cpp

@@ -34,7 +34,7 @@ CHEXA8::CHEXA8() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
 
   su2double oneOnSqrt3 = 0.577350269189626;
 
-  GaussCoord[0][0] = -oneOnSqrt3;  GaussCoord[0][1] = -oneOnSqrt3;  GaussCoord[0][2] = -oneOnSqrt3;	 GaussWeight(0) = 1.0;
+  GaussCoord[0][0] = -oneOnSqrt3;  GaussCoord[0][1] = -oneOnSqrt3;  GaussCoord[0][2] = -oneOnSqrt3;  GaussWeight(0) = 1.0;
   GaussCoord[1][0] =  oneOnSqrt3;  GaussCoord[1][1] = -oneOnSqrt3;  GaussCoord[1][2] = -oneOnSqrt3;  GaussWeight(1) = 1.0;
   GaussCoord[2][0] =  oneOnSqrt3;  GaussCoord[2][1] =  oneOnSqrt3;  GaussCoord[2][2] = -oneOnSqrt3;  GaussWeight(2) = 1.0;
   GaussCoord[3][0] = -oneOnSqrt3;  GaussCoord[3][1] =  oneOnSqrt3;  GaussCoord[3][2] = -oneOnSqrt3;  GaussWeight(3) = 1.0;
@@ -54,14 +54,14 @@ CHEXA8::CHEXA8() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
     Eta = GaussCoord[iGauss][1];
     Zeta = GaussCoord[iGauss][2];
 
-    val_Ni = 0.125*(1.0-Xi)*(1.0-Eta)*(1.0-Zeta);		GaussPoint[iGauss].SetNi(val_Ni,0);
-    val_Ni = 0.125*(1.0+Xi)*(1.0-Eta)*(1.0-Zeta);		GaussPoint[iGauss].SetNi(val_Ni,1);
-    val_Ni = 0.125*(1.0+Xi)*(1.0+Eta)*(1.0-Zeta);		GaussPoint[iGauss].SetNi(val_Ni,2);
-    val_Ni = 0.125*(1.0-Xi)*(1.0+Eta)*(1.0-Zeta);		GaussPoint[iGauss].SetNi(val_Ni,3);
-    val_Ni = 0.125*(1.0-Xi)*(1.0-Eta)*(1.0+Zeta);		GaussPoint[iGauss].SetNi(val_Ni,4);
-    val_Ni = 0.125*(1.0+Xi)*(1.0-Eta)*(1.0+Zeta);		GaussPoint[iGauss].SetNi(val_Ni,5);
-    val_Ni = 0.125*(1.0+Xi)*(1.0+Eta)*(1.0+Zeta);		GaussPoint[iGauss].SetNi(val_Ni,6);
-    val_Ni = 0.125*(1.0-Xi)*(1.0+Eta)*(1.0+Zeta);		GaussPoint[iGauss].SetNi(val_Ni,7);
+    val_Ni = 0.125*(1.0-Xi)*(1.0-Eta)*(1.0-Zeta);   GaussPoint[iGauss].SetNi(val_Ni,0);
+    val_Ni = 0.125*(1.0+Xi)*(1.0-Eta)*(1.0-Zeta);   GaussPoint[iGauss].SetNi(val_Ni,1);
+    val_Ni = 0.125*(1.0+Xi)*(1.0+Eta)*(1.0-Zeta);   GaussPoint[iGauss].SetNi(val_Ni,2);
+    val_Ni = 0.125*(1.0-Xi)*(1.0+Eta)*(1.0-Zeta);   GaussPoint[iGauss].SetNi(val_Ni,3);
+    val_Ni = 0.125*(1.0-Xi)*(1.0-Eta)*(1.0+Zeta);   GaussPoint[iGauss].SetNi(val_Ni,4);
+    val_Ni = 0.125*(1.0+Xi)*(1.0-Eta)*(1.0+Zeta);   GaussPoint[iGauss].SetNi(val_Ni,5);
+    val_Ni = 0.125*(1.0+Xi)*(1.0+Eta)*(1.0+Zeta);   GaussPoint[iGauss].SetNi(val_Ni,6);
+    val_Ni = 0.125*(1.0-Xi)*(1.0+Eta)*(1.0+Zeta);   GaussPoint[iGauss].SetNi(val_Ni,7);
 
     /*--- dN/d xi ---*/
 

Common/src/geometry/elements/CTETRA1.cpp

@@ -45,10 +45,10 @@ CTETRA1::CTETRA1() : CElementWithKnownSizes<NGAUSS,NNODE,NDIM>() {
     Eta = GaussCoord[iGauss][1];
     Zeta = GaussCoord[iGauss][2];
 
-    val_Ni = Xi;						  GaussPoint[iGauss].SetNi(val_Ni,0);
-    val_Ni = Eta;						  GaussPoint[iGauss].SetNi(val_Ni,1);
+    val_Ni = Xi;              GaussPoint[iGauss].SetNi(val_Ni,0);
+    val_Ni = Eta;             GaussPoint[iGauss].SetNi(val_Ni,1);
     val_Ni = 1.0-Xi-Eta-Zeta;	GaussPoint[iGauss].SetNi(val_Ni,2);
-    val_Ni = Zeta;					  GaussPoint[iGauss].SetNi(val_Ni,3);
+    val_Ni = Zeta;            GaussPoint[iGauss].SetNi(val_Ni,3);
 
     /*--- dN/d xi, dN/d eta, dN/d zeta ---*/
 

SU2_CFD/src/output/output_physics.cpp

@@ -279,7 +279,7 @@ void COutputLegacy::ComputeTurboPerformance(CSolver *solver_container, CGeometry
     TotalEnthalpyOutIs[nBladesRow + nStages][nSpanWiseSections]     = EnthalpyOutIs[nBladesRow + nStages][nSpanWiseSections] + 0.5*absVel2;
 
     TotalTotalEfficiency[nBladesRow + nStages][nSpanWiseSections]   = (TotalEnthalpyIn[0][config->GetnSpan_iZones(0)] - TotalEnthalpyOut[nBladesRow-1][config->GetnSpan_iZones(nBladesRow-1)]);
-    TotalTotalEfficiency[nBladesRow + nStages][nSpanWiseSections]	 /= (TotalEnthalpyIn[0][config->GetnSpan_iZones(0)] - TotalEnthalpyOutIs[nBladesRow + nStages][nSpanWiseSections]);
+    TotalTotalEfficiency[nBladesRow + nStages][nSpanWiseSections]  /= (TotalEnthalpyIn[0][config->GetnSpan_iZones(0)] - TotalEnthalpyOutIs[nBladesRow + nStages][nSpanWiseSections]);
     TotalStaticEfficiency[nBladesRow +nStages][nSpanWiseSections]   = (TotalEnthalpyIn[0][config->GetnSpan_iZones(0)] - TotalEnthalpyOut[nBladesRow-1][config->GetnSpan_iZones(nBladesRow-1)]);
     TotalStaticEfficiency[nBladesRow +nStages][nSpanWiseSections]  /= (TotalEnthalpyIn[0][config->GetnSpan_iZones(0)] - EnthalpyOutIs[nBladesRow + nStages][nSpanWiseSections]);
     PressureRatio[nBladesRow + nStages][nSpanWiseSections]          = PressureRatio[0][config->GetnSpan_iZones(0)]*PressureOut[0][config->GetnSpan_iZones(0)]/PressureOut[nBladesRow-1][config->GetnSpan_iZones(nBladesRow-1)];